(a)
Keep the bonding jumper (11) and attached bonding clip for the installation.
S 034-012
(16)
Remove the housing (12) and for No. 1 and 4 main tank boost pumps, the gasket seal (8) from the fuel tank.
S 034-013
(17)
Remove the bolts (21), washers (22), and nuts (23) (four locations) that attach the discharge check valve (1) to the housing (12).
S 034-014
(18)
Remove the removal check valve (18).
(a)
Discard the packing.
TASK 28-22-12-404-016
3. Main Tank Boost Pump Housing Installation (Fig. 401)
_________________________________________
A. Parts
~.............................................................................. | AMM | | AIPC | ................. ............................ | FIG | ITEM | NOMENCLATURE | SUBJECT | FIG | ITEM | ................................................................................ | 401 | 9 |Bolt | 28-22-12 | 02 | 20,25 | | | 10 |Washer | | | 30 | | | 12 |Housing | | | 10 | | | 24 |Screw | | | 15 | | | 25 |Washer | | | 30 | 2......…........…...................................…..........….....….........1
B. Consumable Materials
(1)
D00128 Petrolatum - Technical, VV-P-206
(2)
A00745 Sealant - Corrosion Protection, BMS5-142
(3)
A00247 Sealant - Corrosion Protection, BMS5-95 Type 1 (Alternate cap sealant for BMS5-142)
(4)
C00064 Coating - Alodine 600 Chemical conversion coating for aluminum or aluminum alloys, (MIL-C-5541).
(5)
C00307 Corrosion Resistant Finish - BMS 10-20 Type II
C.
References
(1)
AIPC 28-22-12, Fig. 1
(2)
AMM 20-11-14/701, Metal Surfaces
(3)
AMM 51-21-04/701, Alodine Coating
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
28-22-12
ALL ú ú 01 Page 407 ú Feb 15/99
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400
MAINTENANCE MANUAL
(4)
AMM 28-00-00/201, Fuel
(5)
AMM 28-11-00/201, Fuel Tanks
(6)
AMM 28-11-00/801, Fuel Tanks
(7)
AMM 28-11-02/401, Reserve and Main Tank Access Door
(8)
AMM 28-22-03/401, Main Tank Boost Pump Motor/Impeller Unit
(9)
SWPM 20-20-00, Electrical Bond and Ground
D.
Access
(1)
Location Zones 541 Inbd Main Tank (Part), Front Spar to Mid Spar, Left 544 Inbd Main Tank (Part), Mid Spar to Rear Spar, Left 545 Inbd Main Tank (Part), Mid Spar to Rear Spar, Left 641 Inbd Main Tank (Part), Front Spar to Mid Spar, Right 644 Inbd Main Tank (Part), Mid Spar to Rear Spar, Right 645 Inbd Main Tank (Part), Mid Spar to Rear Spar, Right
(2)
Access Panels
544AB Fuel Tank Access Door
545BB Fuel Tank Access Door
545CD Boost Pump Access Door
545DB Boost Pump Access Door
644AB Fuel Tank Access Door
645BB Fuel Tank Access Door
645CB Boost Pump Access Door
645DB Boost Pump Access Door
E.
Procedure
S 434-041
(1)
On the outside of the tank, do these steps:
(a)
Clean the mating surface of the spar where the bolts go through the structure (AMM 20-11-14/701).
(b)
Prepare the faying surfaces of these components for an electrical surface bond (SWPM 20-20-00) (View A-A): 1) Structure where the bonding jumper attaches 2) Bonding jumper faying surface 3) For the No. 1 and 4 main tank boost pumps, faying surfaces
of the ring (28).
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
28-22-12
ALL ú ú 01 Page 408 ú Feb 15/99
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400
MAINTENANCE MANUAL
S 434-042
(2) On the inside of the tank, clean the mating surfaces of the spar and the housing flange (AMM 20-11-14/701).
S 434-017
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址:747-400 AMM 飞机维护手册 燃油 FUEL 3(53)